Control-effect enhancement of tiltable aircraft stabilizing memb

Details Control-effect enhancement of tiltable aircraft stabilizing memb Control-effect enhancement of tiltable aircraft stabilizing memb

1980-08-05

1983-04-26

Frankfort, Charles E.

Aeronautics and astronautics

Aircraft control

Rudders and empennage

244 45R, 244 48, 244130, 244198, 244218, B64C 516, B64C 2300

Patent

active

043810918

ABSTRACT:
An aircraft having, for example, a tailplane (4, 5) at least part of which is movable with reference to a fuselage (1) to effect control requires the control effect to be enhanced in a certain control position. Accordingly, fixed vanes (8, 9) are provided on the fuselage forward of the tailplane to form a substantially continuous leading edge root extension only when the tailplane is in a given control position.

REFERENCES:
patent: 1814115 (1931-07-01), Blain
patent: 1848037 (1932-03-01), Weick
patent: 2026482 (1935-12-01), Mattioli
patent: 2081957 (1937-06-01), Roche
patent: 3270989 (1966-09-01), Polhamus et al.
patent: 3385538 (1968-05-01), Hodges
patent: 3756529 (1973-09-01), Backlund et al.
patent: 3848831 (1974-11-01), Geary

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